Calculation of Hinge Moments for a Folding Wing Aircraft Based on High-Order Panel Method

Figure 14

Dynamic response during the flight-folding process. (a) Folding angle, (b) angle of attack, (c) altitude, (d) deflection angle of aileron, (e) hinge moment of the inner wing, and (f) hinge moment of the outer wing.

(a)

(b)

(c)

(d)

(e)

(f)